Casualties unknown

2003-12-05: PIPER PA-32-260 (ZS-ELX) — Apron area at Upington Aerodrome e, ZA

Apron area at Upington Aerodrome e, ZA

On December 5, 2003, a PIPER PA-32-260 (registration ZS-ELX) was involved in an aviation accident near Apron area at Upington Aerodrome e, ZA. Investigators recorded the probable cause as: It would appear that the pilot over-primed the engine which resulted in excess fuel in the manifold and in the lower cowling which ignited on starting the engine. The contributing factor would be the high ambient temperature of 43°C. This summary draws on records from the South African Civil Aviation Authority (SACAA) Accident and Incident Investigations Division.

Sourcesthe South African Civil Aviation Authority (SACAA) Accident and Incident Investigations DivisionPrimary reportUpdated 1785709791Data APIEditorial standards

On 5 December 2003, a Piper PA-32-260 (ZS-ELX) suffered an engine fire during start-up at Upington Aerodrome after refueling. Pilot over-priming caused excess fuel ignition; high temperature contributed. No injuries. Fire damage to electrical wiring and harness.

Incident Overview

On 5 December 2003 at 1015Z, a Piper PA-32-260, registration ZS-ELX, experienced an engine fire during start-up on the apron at Upington Aerodrome. The flight was a private operation with two persons on board. No injuries or fatalities were reported. The weather conditions were clear with visibility greater than 10 km, a north westerly wind at 10 knots, and a high ambient temperature of 43°C.

Sequence of Events

The pilot had departed from Cape Town Aerodrome and landed at Upington Aerodrome to refuel en route to Mossel Bay. After the aircraft was refueled to capacity, the pilot initiated the start-up procedure for the continuation of the flight. During start-up, an engine fire started. The pilot responded by selecting the master switch to the off position and vacating the aircraft. Aerodrome personnel then assisted in extinguishing the fire using portable fire extinguishers, successfully limiting the fire to the engine nacelle area.

Damage Assessment

The aircraft sustained fire damage limited to the electrical wiring and ignition harness within the engine nacelle area. The cowlings were slightly burnt and various wires showed signs of fire damage.

Probable Cause

The pilot confirmed to the Approved Maintenance Organisation (AMO) that he had over-primed the engine. This resulted in excess fuel accumulating in the manifold and lower cowling, which ignited upon starting the engine. The high ambient temperature of 43°C was a contributing factor, as it may have increased the volatility of the fuel and reduced the margin for error during start-up.